Logo image
Sign in
Aeroelastic coupling in sonic boom optimization of a supersonic aircraft
Report   Open access

Aeroelastic coupling in sonic boom optimization of a supersonic aircraft

Mariano Vázquez, Alain Dervieux and Bruno Koobus
06/2003

Abstract

UNSTRUCTURED MESH TRANSPIRATION CONDITIONS FLUID/STRUCTURE INTERACTION COMPUTATIONAL FLUID DYNAMICS SHAPE OPTIMAL DESIGN GRADIENT METHOD SHAPE PARAMETRIZATION STEEPEST DESCENT OPTIMIZATION MULTILEVEL OPTIMIZATION ADJOINT METHODS EULER EQUATIONS
In this paper, we consider a multi-disciplinary optimization problem where the initial shape of a wing is sought in order to cope, after elastic deformation by the flow, with some optimality conditions. We propose a medium-strong coupling which allows to consider different softwares communicating a small number of times. Applications to the optimization of the AGARD Wing 445.6 and a flexible supersonic aircraft wing are presented.
url
Find in HALView

Metrics

1 Record Views

Details

Logo image